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CEAS EuroGNC 2024

Experimental Aided Inertial Estimation of Wing Shape for Flexible Aircraft Control

Rajashree Srikanth Graduate Student, ISAE-SUPAERO, Université de Toulouse, Toulouse, France.
Inês M. G. S. Afonso Graduate Student, ISAE-SUPAERO, Université de Toulouse, Toulouse, France.
Leandro R. Lustosa Associate Professor, ISAE-SUPAERO, Université de Toulouse, Toulouse, France.
Abstract:
This paper exhibits an instrumented flexible wing mockup demonstrating a wing shape estimation technique for automatic structural/flight control of very flexible aircraft undergoing large and geometrically nonlinear wing deflections. The proposed method exploits data fusion, using an extended Kalman filter, between distributed rate gyros across the wing and a sighting device at the wing root, and does not require knowledge of strain-displacement curves or specific aircraft dynamic models. The experiment is conducted in a motion capture room for ground truth availability and shows, as predicted in previous work, that the resulting estimation errors are bounded and have promising frequency response.
Keywords: Very Flexible Aircraft; Wing Shape Estimation; Kalman Filtering; Aeroelasticity
View PDFCEAS-GNC-2024-041


Rajashree Srikanth, Inês M. G. S. Afonso, Leandro R. Lustosa: Experimental Aided Inertial Estimation of Wing Shape for Flexible Aircraft Control. Proceedings of the 2024 CEAS EuroGNC conference. Bristol, UK. June 2024. CEAS-GNC-2024-041.
BibTeX entry:

@Incollection{CEAS-GNC-2024-041,
    author = {Srikanth, Rajashree and Afonso, Inês M. G. S. and Lustosa, Leandro R.},
    title = {Experimental Aided Inertial Estimation of Wing Shape for Flexible Aircraft Control},
    booktitle = {Proceedings of the 2024 {CEAS EuroGNC} conference},
    address = {Bristol, UK},
    month = jun,
    year = {2024},
    note = {CEAS-GNC-2024-041}
}